B747 Propulsion

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    Propulsion System of Boeing 747

    Group Members:

    Shamsuddin

    Mustazly

    Hidayat

    Pearl

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    What is Boeing 747?

    Also know as B-747 or B747

    Used for crossing oceans

    Double decked plane

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    Exterior View

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    Interior View

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    Cross Section View

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    TURBOFAN

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    What is Turbofan ?

    Designed as a compromised between the

    turboprop (fuel efficient but noisy) and turbojet

    (powerful yet thirsty)

    Has large internal propeller or ducted fan and two

    streams of air flowing in the engine.

    Main stream goes into all of the components like a

    turbojet

    The secondary flow passes through the fan and is

    either ducted through a second nozzle or mixed

    back with the main stream leaving the turbine.

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    Can be classified as:

    Mixed or unmixed

    Low or high by passSingle, two or three spool

    With or without after burning

    Geared or ungeared

    Nuclear of non-nuclear

    Characteristics:

    Widely used today

    Capable of medium to high thrust

    Capable of supersonic speed

    Better fuel efficiency

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    THE WORKING

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    1. The fan will suck the air into compressor.

    2. The compressor will squeeze and compress the air.

    3. The air will be mixed with oil and burn inside the combustion chamber.

    4. The air will be force out into the turbine and power the turbine to rotate.

    5. The turbine will power the compressor to rotate.

    6. The air will be blown outside the nozzle.

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    Animation of a 2-spool, high-bypass

    turbofan.A. Low pressure spool

    B. High pressure spool

    C. Stationary components

    1. Nacelle

    2. Fan

    3. Low pressure compressor4. High pressure compressor

    5. Combustion chamber

    6. High pressure turbine

    7. Low pressure turbine

    8. Core nozzle

    9. Fan nozzle

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    Type of engines

    High bypassLow bypass

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    Engine Series

    General Electric (GE)

    CF6 - Type of engine: High bypass turbofan

    - Thrust range : 40,000 - 72,000 lbs.

    - Introduction : 1971

    Rolls Royce

    RB211-524 - Type of engine: High bypass turbofan

    - Thrust range: 37,400 - 60,600lbs

    - Introduction: 1997

    Pratt & Whitney

    JT9D-7 - Type of engine: High bypass turbofan

    - Thrust range: 46,300 - 50,000 lbs

    - Introduction: 1970

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    1. Horsepower of 1 Engine125,000hp

    3. Average altitude35,00037,000 feet

    2. Maximum altitude45,100 feet

    4. How far can B747 fly?7,260 nm

    (13,450km)

    5. How long can B747 fly? 16 to 19 hours

    with fuel saving6. How far can B747 glide without fuel?

    - At Altitude 42,000 ft136 miles

    - At Sea Level100miles

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    7. Only B747-400 from B747 family have afterburner.

    8. Life span of an B747 aircraft- Average 25 to 30 years (large number of cycles)

    ** Others - 20 years (small number of cycles)

    9. B747s engines are mixed nozzle

    10. The 747-400 was touted as the fastest subsonic

    commercial airliner in service (913km/h).- Cruised at 0.85 Mach (85 % of the speed of sound)

    - Pratt & Whitney, generated the most powerful 747-

    400 engine with 63,300 lb (28,712 kg) thrust each

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    Die!!!!

    Hahaha..

    Just kidding ^^

    Still able to proceed

    to your destination

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    Why?

    Alight 747 can stay with only two engines, but

    not a heavy one. The one engine is needed to

    power the hydraulics.

    Which mean a B747 still able to fly with 3

    engines.

    Thenwhy need 4 engines??Backup

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    Model Certification First Airline in service Last Delivery747-100/SR/B 30/12/69 Pan Am 9/86

    Japan Air Lines

    747-200 23/12/70 KLM 12/90USAF747-200F 03/07/72 Lufthansa 11/91

    Nippon Cargo

    747-200C 24/07/73 World Airways 9/88Martinair

    747SP 04/02/76 Pan Am 12/09/89Abu Dhabi Govt.

    747-200M 03/07/75 Air Canada12/09/89 -

    Abu Dhabi Govt. (UAE)

    747-300M 03/05/83 Swissair 9/90Sabena

    747-300/SR 03/07/83 Swissair 10/88Japan Asia

    747-400 01/10/89 Northwest747-400M 01/10/89 KLM 04/10/02

    KLM

    747-400D 10/10/91 Japan Air Lines 12/95All Nippon Airways

    747-400F 22/10/93 Cargolux 5/7/09Nippon Cargo Airlines

    747-400ER 29/10/02 Qantas 7/30/03Qantas

    747-400ERF `16/10/02 Air France 11/10/09LoadAir Cargo

    747-8F 19/08/11 Cargolux747-8 14/12/12 Lufthansa

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    ENGINE TYPE

    Pratt & Whitney (PW)

    General Electric (GE)

    Rolls-Royce (RR)

    ENGINE MODEL

    PW JT9D-7A/-7F/-7J

    RR RB211-524B2

    GE CF6-45A2 (747SR)

    ENGINE SPEC

    Max speed : 967km/h(522knot) ; Mach 0.89

    Cruising speed :907km/h (490knot) ;Mach 0.84

    Engine thrust :

    PW 46,500 lbf, (207kN),

    RR 50,100 lbf, (223 kN)

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    ENGINETYPE

    Pratt & Whitney

    (PW)

    General Electric(GE)

    Rolls-Royce (RR)

    ENGINEMODEL

    PW

    JT9D-7R4G2

    GE

    CF6-50E2

    RR

    RB211-524D4

    ENGINESPEC

    Max speed : 967km/h(522knot) ; Mach 0.89

    Cruising speed : 907km/h(490knot) ; Mach 0.84

    Engine thrust :

    PW 54,750 lbf (244 kN)

    GE 52,500 lbf (234 kN)

    RR 53,000 lbf (236 kN)

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    ENGINE TYPE

    ENGINE MODEL

    ENGINE SPEC

    Pratt & Whitney (PW)

    General Electric (GE)

    Rolls-Royce (RR)

    PW JT9D-7R4G2

    GE CF6-80C2B1

    RR RB211-524D4

    Max speed : 967km/h (522knot) ; Mach0.89

    Cruising speed : 907km/h (490knot) ;Mach 0.84

    Engine thrust :

    PW 54,750 lbf (244 kN)

    GE 55,640 lbf (247 kN)

    RR 53,000 lbf (236 kN)

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    ENGINE TYPE

    Pratt & Whitney (PW)

    General Electric (GE)

    Rolls-Royce (RR)

    ENGINE MODEL

    PW 4062

    GE CF6-80C2B5F RR RB211-524G/H

    ENGINE SPEC

    Max speed : 988 km/h

    (533 knots) ; Mach 0.85

    Cruising speed : 912km/h

    (493knots); Mach 0.92

    Engine thrust :

    PW 63,300 lbf (282 kN)

    GE 62,100 lbf (276 kN)

    RR 59,500/60,600lbf

    (265/270 kN)

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    EN

    GINETY

    PE

    GeneralElectric (GE)

    ENG

    INEMOD

    EL

    GEnx-2B67

    EN

    GINESP

    EC

    66,500 lbf(296 kN)

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    References Ronald D.Flackn, Fundamentals of Jet Propulsion with

    Application, Cambridge Aerospace Series, 2005. Thomas A. Ward, Aerospace propulsion Systems,John

    Wiley & Sons (Asia) Pte Ltd, 2010

    http://www.boeing.com/boeing/commercial/747family/pf/pfdomestic_prod.page

    http://wiki.answers.com/Q/Average_flying_height_for_a_Being_747_in_miles#slide4

    http://www.pw.utc.com/JT9D_Engine

    http://www.rolls-royce.com/civil/products/largeaircraft/rb211_524/

    http://www geaviation com/